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Hinchliff, S. (author), Jones, J.W. (author)The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.report 1955
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Jagaciak, J. (author), Ae, D.C. (author), Jones, J.W. (author)Test castings were designed to produce data which would help in the production of gas turbine blades as castings. For castings in H. R. Crown Max the investigation is limited to the effect of subsonic frequencies and range of amplitudes; but in the experiments conducted on Nimonic C. 75, both sub-sonic and sonic ranges of frequency were...report 1955
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- Jones, C.E. (author) report 1961
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Jones, J.G. (author)This paper is concerned with pressure distributions on the wing of a centrally-mounted-wing body combination due to antisymmetric body shaping in the case where the leading edge is subsonic and the body shaping produces flow round the leading edge. The results are used to discuss the limitations of a method for designing body shaping for lifting...report 1961
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Moore, K.C. (author), Jones, J.G. (author)A formula for the supersonic velocity field in terms of a given surface distribution of sources is applied to points lying in the surface. An equation giving the camber shape of a quasi circular-cylindrical surface in terms of a prescribed thickness distribution is derived and the half ring wing with prescribed thickness distribution is...report 1962
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Moore, K.C. (author), Jones, J.G. (author)The design of half-ring wing-body combinations with prescribed wing loadings at supersonic speeds is discussed. A particular load distribution, that behaves near a side edge like the square of the distance from the edge, is considered in detail. In addition to finding wing and optimum body shapes, wave and vortex drag and wing pressure...report 1962
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Jones, J.G. (author)A method is presented for designing the lower surface of a lifting configuration for high supersonic speeds using the known flow field past a nonlifting circular cone. The leading edge can be prescribed on the conical shock wave and the lower surface is obtained by replacing the stream surface through this leading edge by a solid surface....report 1963
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Ham, A.C. (author), Jones, R.E. (author)The effect of radiation of up to 10 kW/ft² intensity al the accuracy with which 33 s.w.g. chromel-alumel thermocouples can be used to measure the surface temperature of mild steel sheets is examined. The error increases with radiation intensity, and under the conditions of the experiments was found to be about 0.3º C per kW/f².report 1963
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Cooke, J.C. (author), Jones, O.K. (author)Certain three-dimensional surfaces studied by Townend have the property that at every streamwise section a supersonic air stream is compressed isentropically in the form of a reversed Prandtl-Meyer flow. If all the compressions are centred on points lying on one straight line the flow is conical. Such a surface may be of use as an engine intake....report 1964
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Jones, D.A. (author), Reason, B.R. (author)The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.report 1964
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Jones, J.G. (author)The response te the lateral oomponent of turbulance of an airoraft with a saturating yaw-damper is investigated. Booton's concept of the equivalent gain of a non-linear element is used in finding the variation of root mean square amplitude of aircraft response with root mean Sqpare gust level. In addition the spectral distortion due to non...report 1965
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Zbrozek, J.K. (author), Jones, J.G. (author)The buffet loads occurring during a transient incursion into the buffet regime due either to a gust or a manoeuvre are briefly discussed. Review of the experimental evidence suggests that although there are substantial effects of the rate of change of incidence on the value of CLmax there is no real evidence that buffet boundaries behave in the...report 1965
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Addicott, E.W. (author), Jones, R.W. (author)An analogue computer programme was derived, making as few approximations as possible, for the calculation of the flight path of an aircraft leaving the end of a ship-borne catapult. Using his 'complete' calculation, it was shown that, for most aircraft, other approximations could be made without significantly impairing the accuracy of the result...report 1966
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- Shen, P.S. (author), Jones, D.J. (author) report 1967
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Shen, P.S. (author), Jones, D.J. (author)The incompressible, three-dimensional, laminar boundary layer flow on a flat plate about a half-cone protuberance has been investigated bath by experiment in the NAE water tunnel and by analysis using Cooke's small cross-flow momentum integral method. Three half cones of semi-apex angles 7½, 10° and 12½, were tested at a Reynolds number of 2 x...report 1967
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- Jones, D.J. (author) report 1968
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Jones, J.G. (author)This Report extends earlier work employing the concept of a self-similar random process in relation to the problem of predicting aircraft gust loads. A discrete gust model of the atmosphere is presented which allows a description of the statistical properties of intense gusts as a function of gust length. Empirical functions describing the...report 1969
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Jones, A.F. (author), Grey-Wilson, P.V. (author), Slooff, J.W. (author)Data are presented from calculations for the surface pressure distribution on some particular swept wings vrith Uarren 12 planform. The calculations were made using the method described in Royal Aeronautical Society Transonic Data Memorandum 6312. Comparisons are given between results obtained from an RAE computer program and a similar program...report 1969
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- Jones, R.T. (author) report
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- Jones, E.B. (author), Webster, B.N. (author), Birmingham, R.W. (author), Roskilly, A.P. (author) report